Air Cargo Unit Load Devices - Performance Requirements and Test Parameters
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint requirements of Title 14 CFR Part 25, except for the 9.0-g forward ultimate inertia force of § 25.561 (b)(3)(ii).
After publication of AS36100B (2016-06), it was decided to add ULD configurations and restraint conditions for 55 x 96 inches (U) and 125 x 196 inches (T) nominal base sizes in Sections 7, “ULD Configurations," and 8, “Testing Restraint Conditions." Further, words have been added to 3.5, “Classification Identifier," to describe requirements regarding dual certification and orientation depiction for RC Q has been corrected.
Revision C is proposed for reference by future TSO-C90 revisions.
Center of gravity (CG)
Industrial vehicles and equipment
Also known as: SAE AS 36100
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